View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 57047U 26145.16144389 +.00000000 +00000-0 +14215-3 0 00006
2 57047 96.7934 207.1516 0008341 192.8411 167.2658 16.01019629 07
| Epoch (UTC): | 25 May 2026 03:52:28 |
| Eccentricity: | 0.0008341 |
| inclination: | 96.7934° |
| perigee height: | 266 km |
| apogee height: | 277 km |
| right ascension of ascending node: | 207.1516° |
| argument of perigee: | 192.8411° |
| revolutions per day: | 16.01019629 |
| mean anomaly at epoch: | 167.2658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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